Accession Number:

AD0612733

Title:

A METHOD FOR CALCULATING THE INTERACTION OF A BOW SHOCK OF A RE-ENTRY VEHICLE AND A BLAST WAVE,

Personal Author(s):

Corporate Author:

PICATINNY ARSENAL DOVER N J FELTMAN RESEARCH LABS

Report Date:

1964-02-01

Abstract:

A general technique for computing the transient flow field in the nose region of a blunt body traveling at hypersonic speeds after being intercepted head-on by a shock wave is presented. The method is not limited to the assumption that the density, pressure and velocities are constant in the interaction region which has been the assumption in previous investigations of this problem. The technique can be applied to compute the flow in the entire interaction region, but is discussed here for computing the low near the axis of symmetry. Author

Pages:

0018

Descriptors:

File Size:

0.00MB

Full text not available:

Request assistance